CN109983220A - Radial reactionary style wind turbine generator/power device/Kumars RR VT engine - Google Patents

Radial reactionary style wind turbine generator/power device/Kumars RR VT engine Download PDF

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Publication number
CN109983220A
CN109983220A CN201680090739.3A CN201680090739A CN109983220A CN 109983220 A CN109983220 A CN 109983220A CN 201680090739 A CN201680090739 A CN 201680090739A CN 109983220 A CN109983220 A CN 109983220A
Authority
CN
China
Prior art keywords
engine
engine according
kumars
wind turbine
radial
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201680090739.3A
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Chinese (zh)
Inventor
苏库马兰巴拉纳丹
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Individual
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Individual
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Publication date
Application filed by Individual filed Critical Individual
Publication of CN109983220A publication Critical patent/CN109983220A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/04Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • F03D3/0409Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels surrounding the rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/002Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  the axis being horizontal
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/005Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  the axis being vertical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06Rotors
    • F03D3/061Rotors characterised by their aerodynamic shape, e.g. aerofoil profiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/10Stators
    • F05B2240/12Fluid guiding means, e.g. vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/21Rotors for wind turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/40Use of a multiplicity of similar components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/20Geometry three-dimensional
    • F05B2250/25Geometry three-dimensional helical
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/74Wind turbines with rotation axis perpendicular to the wind direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E70/00Other energy conversion or management systems reducing GHG emissions
    • Y02E70/30Systems combining energy storage with energy generation of non-fossil origin

Abstract

A kind of small-sized self-tolerant engine using wind-power electricity generation.Every engine can run 2 generators simultaneously.Multiple engine units can be installed for large scale business purposes.

Description

Radial reactionary style wind turbine generator/power device/Kumars RR VT engine
Technical field
This engine is the kinetic energy using wind and the field device for being translated into electric energy.
Background technique
In view of the severe situation of current global warming, it is necessary to find a kind of cheap and clean energy.It must also be one The sustainable renewable energy of kind.Answer is wind energy.
For many years, the mankind carry out machine work using wind energy always.The windmill of early stage is for the wheat and from canal of milling Water intaking.
In recent years, people are more and more interested in wind turbine electric generation, innovate also more and more.It is most common in the world It is the wind tower for being equipped with propeller blade.These towers and its blade are huge.Build the cost of these wind turbine towers too Gao Liao.The theory of this and the cheap energy runs in the opposite direction, and the construction cost of the cheap energy can pass on to consumers.Building them is one Item difficult task, maintenance are got up pretty troublesome.One generator is connected with one group of propeller.Therefore, one generator of a tower.
Also occur some novel designs recently, these designs seemingly artistry in itself, rather than service In actual purpose.
Summary of the invention
I thinks that this invention is the Rolls Royce in all wind turbine generators, it meets very high expectation.Two Platform generator can be run simultaneously by an engine unit.
Developing concept used by this engine is to be based on:
(a) bernoulli principle --- using special-shaped outline (profiled contours) and pass through different surfaces region Constricted path channel on air-flow pressure and speed substantial connection.With
(b) a kind of improved Archimedian screw generates helical blade using arc tangent design function.Single continous way leaf Piece is connected on turbine rotor with 45 to an angle of 90 degrees.
In conjunction with above-mentioned (a) and (b), vortex shape air-flow can be formed in peritrochanteric.The pitch of blade on turbine rotor It is variation, i.e. rise/fall, to generate barometric gradient.This design feature forces the air between blade wall to flow.
The basic element of character of Kumars RR VT engine has:
(1) pipeline/casing assembly
The shell (shell can be referred to as pipeline below) of engine allows open end of the air by it.At the top of pipeline It is the tie point of two aerofoil profiles (aerofoils) with pedestal.Side wall acts also as the support knot of turbine rotor, axis, axle journal and bearing Structure.
(2) turbine rotor, blade and shaft assembly
Rotor is the pedestal for connecting blade and end plate.It is also the shell of turbine wheel shaft.
Single continous way blade on rotor between rotor and end plate helically arrange by mode (whorl pattern). According to the difference of position, blade lean 45 to 90 is spent.It means that at the time of any given, vaned a part always Optimal Windward angle can be reached.This can cause a lift, so as to cause go to action.The spiral of blade is using change pitch Arc tangent design.
Axis supports rotor assembly, axle journal, bearing and gear, and gear is for connecting generator.
(3) aerofoil profile
The aerofoil profile that two angles of attack are 10 degree in pipeline for forming low-pressure area.Up-front chord angle (the chord of aerofoil profile It angle) is 45 degree.This is to make wind towards the center of rotor assembly to create an ascending air.
(4) bearing and gear assembly
Bearing is used to support turbine rotor and shaft assembly together with axle journal.Gear is connected to turbine the tip of the axis, for Generator connection.
The combination of above-mentioned component and its position for Kumar RR VT engine realize high torque and it is high-revolving most Good efficiency is most important.
Since the structure of engine is only made of several components, easy to manufacture, unquestionably, engine is very hard Gu.
Component explanation and operating pressure figure
Attached drawing will be apparent from Kumar RR VT engine and its working principle.
Fig. 1 shows the front view of engine;
Fig. 2 shows [A-A] sectional views of engine;And
Fig. 3 shows the operating pressure of engine interior generation.
According to diagram, Fig. 1, Fig. 2 and Fig. 3 are explained itself.
From figure 3, it can be seen that air is invariably prone to flow to area of low pressure from high-pressure area.This movement is so that pass through hair The air momentum of motivation increases.
Claims (according to the 19th article of modification of treaty)
1. a kind of engine, for using wind energy and converting wind energy into electric energy.
2. engine according to claim 1 utilizes variation (Fig. 3) Lai Yunhang of the engine interior pipeline pressure Turbine.
3. engine according to claim 2 reaches required pipeline pressure, the fixed dress using fixed device Set e.g. aerofoil profile, cylinder, turbo blade and end plate.
4. engine pack according to claim 3 diplomatic must be placed.The wind entered from engine front or rear portion Turbine direction of rotation will not be changed.
5. engine according to claim 4 may be mounted on firm pedestal, and may be mounted at anyly Side, whether land, in the sea or aerial.
6. engine according to claim 5 is connect by the gear train on end with 2 generators, to keep dynamic Balance, static balance and stability.
7. engine according to claim 6 is specified for industry/private use since size is big, needs to install On firm pedestal.
8. engine according to claim 7, can be horizontal, vertical or in any required position installation.

Claims (8)

1. a kind of engine, for using wind energy and being translated into electric energy.
2. engine according to claim 1 is operated using pressure change (Fig. 3).
3. engine according to claim 2 reaches required pressure using fixed device, the fixed device is for example It is aerofoil profile (1), cylinder (4), turbo blade (3) and end plate (5).
4. component according to claim 3 diplomatic must be placed, to meet claim 2.
5. engine according to claim 4 may be mounted on pedestal (9), and may be mounted at Anywhere.
6. engine according to claim 5 is connected with 2 generators in the end of turbine wheel shaft (6) by gear (8) system It connects.
7. engine according to claim 6 can be used as multiple units and run in single location or multiple positions, and And output can be it is local or concentration.
8., can be horizontal, vertical or in any required position installation according to engine described in claim 6 and 7.
CN201680090739.3A 2016-10-12 2016-10-12 Radial reactionary style wind turbine generator/power device/Kumars RR VT engine Pending CN109983220A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/MY2016/000063 WO2018070862A1 (en) 2016-10-12 2016-10-12 Radial reaction wind turbine engine / powerplant / kumars rr vt engine

Publications (1)

Publication Number Publication Date
CN109983220A true CN109983220A (en) 2019-07-05

Family

ID=61905738

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201680090739.3A Pending CN109983220A (en) 2016-10-12 2016-10-12 Radial reactionary style wind turbine generator/power device/Kumars RR VT engine

Country Status (4)

Country Link
US (1) US20190242360A1 (en)
EP (1) EP3526470A4 (en)
CN (1) CN109983220A (en)
WO (1) WO2018070862A1 (en)

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CN1900514A (en) * 2006-07-14 2007-01-24 单建锡 Horn mouth drum type screw wind power generator
CN201270451Y (en) * 2008-05-08 2009-07-08 崔文安 Self-boosting magnetic field rotation type wind-magnet synthetic electricity generator
CN102011683A (en) * 2010-12-21 2011-04-13 青岛敏深风电科技有限公司 Spiral turbine blade and vortex convective wind power generator
CN203759947U (en) * 2014-03-05 2014-08-06 张风吉 Experimental device for demonstrating energy conversion
US20150017006A1 (en) * 2012-03-12 2015-01-15 The Power Collective Ltd. Wind Turbine Assembly
CN104454384A (en) * 2014-11-14 2015-03-25 无锡信大气象传感网科技有限公司 Foreign matter prevention electric generator
CN104854325A (en) * 2012-12-27 2015-08-19 三菱重工业株式会社 Radial turbine rotor blade
CN205423073U (en) * 2016-03-03 2016-08-03 高飞 Wind power generation machine of spiral shell shape structure
WO2016145520A1 (en) * 2015-03-16 2016-09-22 O'hagan Peter K Improved wind turbine suitable for mounting without a wind turbine tower

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US6638005B2 (en) * 2002-01-17 2003-10-28 John W. Holter Coaxial wind turbine apparatus having a closeable air inlet opening
US7695242B2 (en) * 2006-12-05 2010-04-13 Fuller Howard J Wind turbine for generation of electric power
GB0912695D0 (en) * 2009-07-22 2009-08-26 Power Collective The Ltd A generator
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* Cited by examiner, † Cited by third party
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CN1900514A (en) * 2006-07-14 2007-01-24 单建锡 Horn mouth drum type screw wind power generator
CN201270451Y (en) * 2008-05-08 2009-07-08 崔文安 Self-boosting magnetic field rotation type wind-magnet synthetic electricity generator
CN102011683A (en) * 2010-12-21 2011-04-13 青岛敏深风电科技有限公司 Spiral turbine blade and vortex convective wind power generator
US20150017006A1 (en) * 2012-03-12 2015-01-15 The Power Collective Ltd. Wind Turbine Assembly
CN104854325A (en) * 2012-12-27 2015-08-19 三菱重工业株式会社 Radial turbine rotor blade
CN203759947U (en) * 2014-03-05 2014-08-06 张风吉 Experimental device for demonstrating energy conversion
CN104454384A (en) * 2014-11-14 2015-03-25 无锡信大气象传感网科技有限公司 Foreign matter prevention electric generator
WO2016145520A1 (en) * 2015-03-16 2016-09-22 O'hagan Peter K Improved wind turbine suitable for mounting without a wind turbine tower
CN205423073U (en) * 2016-03-03 2016-08-03 高飞 Wind power generation machine of spiral shell shape structure

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Also Published As

Publication number Publication date
EP3526470A1 (en) 2019-08-21
US20190242360A1 (en) 2019-08-08
WO2018070862A1 (en) 2018-04-19
EP3526470A4 (en) 2020-05-27

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Application publication date: 20190705

RJ01 Rejection of invention patent application after publication